U.S. patent application number 13/160449 was filed with the patent office on 2011-10-06 for proximity detection method for magnetic head and recording medium.
This patent application is currently assigned to Kabushiki Kaisha Toshiba. Invention is credited to Richard M. EHRLICH, Craig L. TOMITA.
Application Number | 20110242955 13/160449 |
Document ID | / |
Family ID | 43465133 |
Filed Date | 2011-10-06 |
United States Patent
Application |
20110242955 |
Kind Code |
A1 |
EHRLICH; Richard M. ; et
al. |
October 6, 2011 |
PROXIMITY DETECTION METHOD FOR MAGNETIC HEAD AND RECORDING
MEDIUM
Abstract
Touchdown between a read/write head of disk drive and a
recording medium is detected based on the variance in the frequency
domain of position error signals (PES), each of which is measured
after incrementally positioning the read/write head closer to the
recording medium, from a baseline PES. The synchronous portion of
the baseline PES is quantified and removed from the baseline PES
and subsequent PES measurements to remove the effect of the
synchronous portion of the baseline PES. The non-synchronous
portion of the PES measured at a particular read/write head
position may also be removed by synchronously averaging multiple
PES measurements for each read/write head position. Detection of
touchdown may be based on the rate of change of the variance in the
frequency domain of PES relative to a baseline PES, instead of the
absolute value of the variance.
Inventors: |
EHRLICH; Richard M.;
(Saratoga, CA) ; TOMITA; Craig L.; (Pleasanton,
CA) |
Assignee: |
Kabushiki Kaisha Toshiba
Tokyo
JP
|
Family ID: |
43465133 |
Appl. No.: |
13/160449 |
Filed: |
June 14, 2011 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
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13031590 |
Feb 21, 2011 |
8004788 |
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13160449 |
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12504430 |
Jul 16, 2009 |
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13031590 |
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Current U.S.
Class: |
369/53.39 ;
G9B/27.052 |
Current CPC
Class: |
G11B 5/6005 20130101;
G11B 27/36 20130101; G11B 20/10203 20130101; G11B 20/10351
20130101; G11B 2220/2516 20130101; G11B 20/10009 20130101 |
Class at
Publication: |
369/53.39 ;
G9B/27.052 |
International
Class: |
G11B 27/36 20060101
G11B027/36 |
Claims
1. A method for detecting touchdown between a magnetic head and a
recording medium, comprising: measuring a baseline position error
signal of the magnetic head with the magnetic head at a baseline
position; determining a synchronous portion of the baseline
position error signal; generating an adjusted baseline position
error signal by removing the synchronous portion of the baseline
position error signal from the baseline position error signal;
measuring additional position error signals of the magnetic head
with the magnetic head positioned successively closer to the
recording medium with each additional measurement; generating an
adjusted position error signal for each of the additional position
error signals by removing the synchronous portion of the baseline
position error signal from a synchronous portion of the additional
position error signal; converting the adjusted baseline position
error signal and each of the adjusted position error signals from a
time domain into a frequency domain; and detecting touchdown based
on a combined variance value that is computed from variances in the
adjusted position error signals with respect to the adjusted
baseline position error signal at each of a discrete number of
frequencies that are within one or more selected frequency bands in
the frequency domain.
2. The method according to claim 1, further comprising: driving the
magnetic head from a baseline position to a first position that is
closer to the recording medium than the baseline position and then
measuring the additional position error signal with the magnetic
head at the first position; and driving the magnetic head from the
first position to a second position that is closer to the recording
medium than the first position and then measuring the additional
position error signal with the magnetic head at the second
position.
3. The method according to claim 2, further comprising: until
touchdown is detected, driving the magnetic head to positions that
are successively closer to the recording medium and then measuring
the additional position error signals at said positions.
4. The method according to claim 1, wherein the combined variance
value is a sum total of each of said variances.
5. The method according to claim 4, wherein each variance in the
position error signals is a variance between one of the adjusted
position error signals and the adjusted baseline position error
signal at a particular frequency within the one or more selected
frequency bands.
6. The method according to claim 5, wherein the touchdown is
detected when the difference between the average combined variance
value for the most recent N measurements and a baseline average
exceeds a predetermined threshold, where N is two or more.
7. The method according to claim 1, wherein the synchronous portion
of an additional position error signal is determined by measuring
the position error signal for two or more revolutions and averaging
the measured position error signals over said two or more
revolutions.
Description
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application is a divisional of U.S. patent application
Ser. No. 13/031,590, filed Feb. 21, 2011, which is a divisional of
U.S. patent application Ser. No. 12/504,430, filed Jul. 16, 2009,
the entire contents of which are incorporated herein by
reference.
BACKGROUND OF THE INVENTION
[0002] 1. Field of the Invention
[0003] Embodiments of the present invention relate generally to
magnetic disk drives and, more particularly, to a proximity
detection method for a magnetic head and a recording medium.
[0004] 2. Description of the Related Art
[0005] In a hard disk drive (HDD), the spacing between a magnetic
recording head and magnetic storage disk, referred to as "head
clearance," is a critical performance parameter. Reducing head
clearance during reading and writing operations can reduce bit
error rate and allow accurate storage and retrieval of data that
are stored on a disk at very high linear densities. Dynamic
fly-height (DFH) control of read/write (R/W) heads is commonly used
by modern HDDs to allow low enough fly heights for high-density
storage media while maintaining sufficient head clearance over
different head locations and disk drive temperatures.
[0006] For proper operation of an HDD, DFH control schemes
generally require some form of calibration to determine how the fly
height of an R/W head varies with stroke location, temperature, and
applied DFH control signal. An important step in calibrating DFH
control is determination of touchdown, i.e., when the R/W head
actually makes contact with the storage medium. During normal
operation such contact is avoided, but as part of calibration,
touchdown provides an absolute benchmark of R/W head position
relative to a disk, and is used in subsequent calibration
procedures. For calibration at a given stroke location and
temperature, the DFH control signal is stepped through increasing
values until a portion of the R/W head begins to contact the disk.
Given the touchdown control level and the actuation efficiency,
i.e., the amount of fly-height change per unit of applied control
signal, a DFH control algorithm can regulate the fly height
accurately for an R/W head as a function of location and
temperature.
[0007] A touchdown-detection algorithm is commonly used to control
the HDD during HDD self-test when determining touchdown. Ideally,
such a touchdown-detection algorithm can be performed by an HDD
without the need for external measurement equipment. When no
external equipment is needed for touchdown determination--other
than the mechanical support and power supply already required for
HDD self-test--the HDD test process is significantly expedited.
This is because the setup and breakdown of each HDD before and
after self-test can remain unchanged, thereby avoiding
complications to the self-test process. In addition, a
touchdown-detection algorithm should reliably determine touchdown.
Declaring a touchdown power that is too low results in the R/W head
flying higher than the optimal height, which can result in poor
read/write quality. Declaring a touchdown power that is too high
results in the R/W head flying lower than the optimal height, which
can result in undesired head/disk contact and failure in the field.
Further, a touchdown-detection algorithm should not require
excessive head/disk contact during the measurement process for
robust calibration of the R/W head position, to minimize the
potential for damage to the R/W head and disk surface.
[0008] There are a number of methods known in the art for
determining touchdown. One approach is to observe the gain of the
read channel variable gain amplifier (VGA) as DFH power is
increased, and declare touchdown when further increases in DFH
power do not produce significant decreases in VGA gain. However, to
detect the point at which VGA gain decreases, the DFH power must be
driven past the point of initial head/disk contact, which is
undesirable. Another approach involves observing acoustic output of
the HDD by placing a microphone near the R/W head and declaring
touchdown when a pre-determined level of acoustic output is
detected. Because installation and removal of the microphone can
significantly complicate setup of an HDD for the self-test process,
this method is also undesirable. Another approach involves
observing overall servo track misregistration (TMR) of the R/W head
as DFH power is increased and declaring touchdown when the TMR
exceeds a specified level. As with the VGA gain approach, accurate
determination of touchdown may require overdriving the R/W head
past the point of initial contact with the disk. Therefore, this
approach is also undesirable for determining touchdown. In another
approach, modulation of the read signal is observed from the R/W
head, and touchdown is declared when a specified level of
modulation is reached. Overdriving of the R/W head past initial
contact with the disk may be necessary for this approach as well.
In yet another approach, variance of position error signal (PES),
either for total PES or specified frequency bands, is observed as a
function of DFH power, and touchdown is declared when the observed
variance exceeds a threshold value. While such an approach can
detect touchdown for some disk drives, it has been demonstrated
that for many disk drives, and even for particular tracks on a
given disk drive, touchdown may not be reliably detected by this
method.
[0009] In light of the above, there is a need for an improved
method of touchdown detection that can be performed by an HDD
during the self-test process without additional measurement
equipment and does not require excessive head/disk contact.
SUMMARY OF THE INVENTION
[0010] One or more embodiments of the invention provide methods for
detecting touchdown between a magnetic head and a recording medium
by evaluating position error signals (PES) in the frequency domain
while incrementally increasing the dynamic fly-height (DFH) control
signal.
[0011] In a first embodiment, touchdown is detected based on
variances in the PES at each of a discrete number of frequencies
that are within one or more selected frequency bands in the
frequency domain, i.e., the PES variance is "band-limited," and the
variance is measured with respect to a baseline PES. The one or
more frequency bands are selected so that portions of the PES
spectrum that either do not change at touchdown or change for
reasons unrelated to touchdown are ignored. In addition, the
synchronous portion of the baseline PES is quantified and removed
from the baseline PES measurement and all subsequent PES
measurements. This has the effect of better isolating the portion
of the PES that is affected by touchdown.
[0012] A method for detecting touchdown between a magnetic head and
a recording medium, according to the first embodiment, comprises
measuring a baseline position error signal of the magnetic head
with the magnetic head at a baseline position, determining a
synchronous portion of the baseline position error signal,
generating an adjusted baseline position error signal by removing
the synchronous portion of the baseline position error signal from
the baseline position error signal, measuring additional position
error signals of the magnetic head with the magnetic head
positioned successively closer to the recording medium with each
additional measurement, generating adjusted position error signals
by removing the synchronous portion of the baseline position error
signal from each of the additional position error signals,
converting the adjusted baseline position error signal and each of
the adjusted position error signals from a time domain into a
frequency domain, and detecting touchdown based on a combined
variance value that is computed from variances in the adjusted
position error signals with respect to the adjusted baseline
position error signal at each of a discrete number of frequencies
that are within one or more selected frequency bands in the
frequency domain.
[0013] In a second embodiment, touchdown is detected based on
variances in the band-limited PES, where the effect of the
synchronous portion of the baseline PES and the non-synchronous
portion of each PES measured at a particular DFH power are removed.
The non-synchronous portion of the PES measured at a particular DFH
power is removed by synchronously averaging multiple PES
measurements for each DFH power. Again, this has the effect of
better isolating the portion of the PES that is affected by
touchdown.
[0014] A method for detecting touchdown between a magnetic head and
a recording medium, according to the second embodiment, comprises
measuring a baseline position error signal of the magnetic head
with the magnetic head at a baseline position, determining a
synchronous portion of the baseline position error signal,
generating an adjusted baseline position error signal by removing
the synchronous portion of the baseline position error signal from
the baseline position error signal, measuring additional position
error signals of the magnetic head with the magnetic head
positioned successively closer to the recording medium with each
additional measurement, generating an adjusted position error
signal for each of the additional position error signals by
removing the synchronous portion of the baseline position error
signal from a synchronous portion of the additional position error
signal, converting the adjusted baseline position error signal and
each of the adjusted position error signals from a time domain into
a frequency domain, and detecting touchdown based on a combined
variance value that is computed from variances in the adjusted
position error signals with respect to the adjusted baseline
position error signal at each of a discrete number of frequencies
that are within one or more selected frequency bands in the
frequency domain.
[0015] In a third embodiment, touchdown is detected based on the
rate of change, i.e., the slope, of band-limited PES variation
after 1) removal of the synchronous portion of the baseline PES or
2) removal of both the synchronous portion of the baseline PES and
the non-synchronous portion of each PES measured at a particular
DFH power.
[0016] A method for detecting touchdown between a magnetic head and
a recording medium, according to the third embodiment, comprises
driving the magnetic head to multiple positions that are
successively closer to the recording medium until touchdown is
detected, determining a position error signal for each of the
multiple positions, converting each of the position error signals
from a time domain into a frequency domain, computing a combined
variance value from variances in the position error signals with
respect to a baseline position error signal at each of a discrete
number of frequencies that are within one or more selected
frequency bands in the frequency domain, and detecting touchdown
when the difference between the average combined variance value for
a group of positions of the magnetic head that are closest to the
recording medium and a baseline average exceeds a threshold value.
The determined position error signal at each of the positions may
be equal to a measured position error signal minus a synchronous
portion of a baseline position error signal, or may be derived from
a synchronous portion of a measured position error signal.
BRIEF DESCRIPTION OF THE DRAWINGS
[0017] So that the manner in which the above recited features of
the present invention can be understood in detail, a more
particular description of the invention, briefly summarized above,
may be had by reference to embodiments, some of which are
illustrated in the appended drawings. It is to be noted, however,
that the appended drawings illustrate only typical embodiments of
this invention and are therefore not to be considered limiting of
its scope, for the invention may admit to other equally effective
embodiments.
[0018] FIG. 1 is a perspective view of a disk drive that can
benefit from embodiments of the invention described herein.
[0019] FIG. 2 illustrates a magnetic storage disk.
[0020] FIG. 3 is a schematic side view of an R/W head positioned
over a surface of magnetic storage disk.
[0021] FIG. 4 sets forth a flow diagram illustrating a baseline RRO
removal method for determining touchdown of an R/W head against a
magnetic storage disk, according to an embodiment of the
invention.
[0022] FIG. 5A is a graph of a series of PES frequency
distributions.
[0023] FIG. 5B sets forth a graph of band-limited PES variance from
a baseline PES measured against DFH power for the spectra in FIG.
5A.
[0024] FIG. 6A is a graph of a series of PES frequency
distributions that are obtained using the baseline RRO removal
method.
[0025] FIG. 6B sets forth a graph of band-limited PES variance from
a baseline PES having the baseline RRO removed, measured against
DFH power for the spectra in FIG. 6A.
[0026] FIG. 7 sets forth a flow diagram illustrating a band-limited
RRO method for determining touchdown of an R/W head against a
magnetic storage disk, according to an embodiment of the
invention.
[0027] FIGS. 8A and 8B illustrate PES frequency distributions, and
a graph of band-limited PES variance measured against DFH power,
respectively.
[0028] FIGS. 9A and 9B illustrate PES frequency distributions
obtained using the baseline RRO removal method, and a graph of
band-limited PES variance measured against DFH power,
respectively.
[0029] FIGS. 10A and 10B illustrate PES frequency distributions
using the band-limited RRO method, and a graph of band-limited PES
variance measured against DFH power, respectively.
[0030] FIG. 11 sets forth a flow diagram illustrating a slope
method for determining touchdown of an R/W head against a magnetic
storage disk, according to an embodiment of the invention.
[0031] FIG. 12 sets forth a graph that illustrates the output of
the slope method, according to an embodiment of the invention.
[0032] For clarity, identical reference numbers have been used,
where applicable, to designate identical elements that are common
between figures. It is contemplated that features of one embodiment
may be incorporated in other embodiments without further
recitation.
DETAILED DESCRIPTION
[0033] The present invention contemplate methods for detecting
touchdown between an R/W head and disk by determining the variance
in the frequency domain of position error signals (PES), each
measured after incrementally increasing the DFH control signal,
from a baseline PES. To quantify the variance in the frequency
domain, a discrete Fourier transform (DFT) of the baseline PES and
of each PES produced for a given DFH control signal is used. In
addition, band-limited PES variance may be used to improve
sensitivity to touchdown, in which the variance is only measured
for a selected portion of the DFT spectrum.
[0034] Embodiments of the invention include a "baseline repeatable
runout (RRO) removal" method, in which the synchronous portion of
the baseline PES is quantified and removed from the baseline PES
measurement and all subsequent PES measurements, a "band-limited
RRO method," in which the non-synchronous portion of the PES
measured at a particular DFH power is removed by synchronously
averaging multiple PES measurements for each DFH power, and a
"slope" method, in which the rate of change of the output of either
the baseline RRO removal or band-limited RRO method is observed.
The baseline RRO removal method is described below in conjunction
with FIG. 4, the band-limited RRO method is described below in
conjunction with FIG. 7, and the slope method is described below in
conjunction with FIG. 11.
[0035] FIG. 1 is a perspective view of a disk drive 110 that can
benefit from embodiments of the invention as described herein. For
clarity, disk drive 110 is illustrated without a top cover. Disk
drive 110 includes a magnetic storage disk 112 that is rotated by a
spindle motor 114. Spindle motor 114 is mounted on a base plate
116. An actuator arm assembly 118 is also mounted on base plate
116, and includes an R/W 120 mounted on a flexure arm 122. Flexure
arm 122 is attached to an actuator arm 124 that rotates about a
bearing assembly 126. Voice coil motor 128 moves R/W 120 relative
to magnetic storage disk 112, thereby positioning R/W head 120 over
the desired concentric data storage track disposed on the surface
112A of magnetic storage disk 112. Spindle motor 114, R/W head 120,
and voice coil motor 128 are coupled to electronic circuits 130,
which are mounted on a printed circuit board 132. Electronic
circuits 130 include a read channel, a microprocessor-based
controller, and random access memory (RAM). For clarity of
description, disk drive 110 is illustrated with a single magnetic
storage disk 112 and actuator arm assembly 118; however, disk drive
110 may also include multiple disks 112 and multiple actuator arm
assemblies 118.
[0036] FIG. 2 illustrates magnetic storage disk 112 with data
organized in a typical manner well known in the art. Magnetic
storage disk 112 includes concentric data storage tracks 242 for
storing data. Each of concentric data storage tracks 242 is
schematically illustrated as a centerline, however each of
concentric data storage tracks 242 occupies a finite width about a
corresponding centerline. Magnetic storage disk 112 includes
radially aligned servo spokes 244, also referred to as servo
wedges, that cross concentric data storage tracks 242 and store
servo information in servo sectors in concentric data storage
tracks 242. The servo information is read by R/W head 120 during
read and write operations to position the head 120 above a desired
track 242. For clarity, a small number of concentric data storage
tracks 242 and servo spokes 244 are shown. Typically, the actual
number of concentric data storage tracks 242 and servo spokes 244
included on magnetic storage disk 112 is considerably larger.
[0037] FIG. 3 is a schematic side view of R/W head 120 positioned
over surface 112A of magnetic storage disk 112. R/W head 120
includes a read head 360, a write head 370, and an air-bearing
surface (ABS) 320, which faces toward surface 112A of magnetic
storage disk 112. The rotation of magnetic storage disk 112 in the
direction of arrow 301 generates an air bearing between ABS 320 of
R/W head 120. During operation of disk drive 110, the air bearing
counterbalances the slight spring force produced by the suspension
of flexure arm 122, thereby holding R/W head 120 a small,
substantially constant fly height 330 above surface 112A. With the
high linear densities now in use for data storage on modern disk
drives, fly height 330 is commonly less than 10 nanometers and may
be as small as 3 nanometers.
[0038] In operation, a thermal or mechanical fly-height actuator
(not shown) disposed on flexure arm 122 varies the vertical
position of R/W head 120 over surface 112A as necessary to maintain
an optimal fly height 330. A fly-height controller contained in
electronic circuits 130 controls the fly-height actuator. The
fly-height controller steps R/W head 120 incrementally closer to or
farther from surface 112A by increasing or decreasing the DFH
control signal applied to the fly-height actuator, where the DFH
control signal can be expressed in digital-to-analog converter
(DAC) counts. The DFH control signal causes thermal dissipation in
the slider. The resulting shape distortion of the slider can bring
the read and write elements closer to the disk surface. For
example, when the applied DFH control signal is at a minimum, i.e.,
zero DAC counts, fly height 330 is at its maximum value. The object
of a touchdown determination algorithm is to quantify the number of
DAC counts applied to the fly-height actuator that result in actual
or imminent contact between R/W head 120 and surface 112A.
[0039] Precise alignment of R/W head 120 over a desired concentric
data storage track 242 is monitored by means of the PES. As is
commonly known in the art, a PES is produced by servo bursts
located in servo spokes 244 when magnetic storage disk 112 is
rotated in proximity to R/W head 120. The PES allows the
microprocessor-based controller in electronic circuits 130 to
determine the position of R/W head 120 relative to a given
concentric data storage track 242. As noted above, embodiments of
the invention contemplate declaring touchdown of R/W head 120 by
any of three different methods, referred to herein as the baseline
RRO removal method, the band-limited RRO method, and the slope
method. Each of these methods include observation of variances in a
band-limited PES spectrum, as opposed to the total PES spectrum,
and are described in turn below.
[0040] Because the methods disclosed herein observe variances in
band-limited PES, only a limited portion of the PES spectrum is
used to determine touchdown. Hence, the remaining portions of the
PES spectrum, which either do not change at touchdown or change for
other reasons unrelated to touchdown, are ignored by the algorithm.
Consequently, sensitivity of the touchdown detection algorithm is
substantially improved. Inventor analysis has determined that the
changes in the PES spectrum that occur at touchdown are found in
the higher frequency region of the spectrum, e.g., between about
one half the Nyquist frequency and the Nyquist frequency of the
PES. Observation has shown that variance in the lower frequency
portions of the PES spectrum, particularly in the frequency range
of 0-2000 Hz, is dominated by other noise sources not associated
with touchdown, including spindle motor vibration (500-800 Hz),
test stand vibration (10s-100s of Hz), and disk-flapping modes and
arm assembly modes (1-2 kHz). In addition, the low frequency
"beating," i.e., the low-frequency modulation of higher-frequency
vibrations (generally in the 10s of Hz), produced by any such
resonant vibration sources that are mechanically coupled and
closely matched in frequency can generate another source of low
frequency variance in PES, such as the 15 Hz beating generated by a
1215 Hz arm assembly vibration mode and a 1230 Hz disk "umbrella"
vibration mode.
[0041] Such lower frequency variance in the PES can be eliminated
by selecting a lower bound to the band-limited PES variation
algorithm, thereby improving the signal-to-noise ratio of the
touchdown algorithm. For example, in one embodiment a disk drive
having approximately 150 servo wedges and rotating at 120 Hz
undergoes touchdown calibration. The PES frequency distribution
used by the baseline RRO removal, the band-limited RRO, or the
slope methods for such a disk drive may include the frequency range
of approximately 5000 Hz to 9000 Hz, the latter of which being the
Nyquist frequency of the disk drive. One of skill in the art will
appreciate that the frequency range of a PES frequency distribution
used for touchdown detection in embodiments of the invention will
vary as a function of the Nyquist frequency of the PES, which can
differ according to the design and operation of a given disk
drive.
[0042] The baseline RRO removal method for determining touchdown is
now described. Inventor analysis has determined that much if not
all of the additional servo track misregistration (TMR) of the R/W
head suffered at touchdown is synchronous with disk revolution.
Hence, any synchronous runout, or RRO, present in the baseline PES
measurement can make detection of touchdown problematic when the
baseline RRO includes frequency components that coincide with the
frequencies that are excited at touchdown. For example, the
baseline RRO can mask touchdown-induced TMR by acting as noise
present at the frequencies of interest for determining touchdown.
Worse, when baseline RRO includes frequency components that
coincide with the frequencies excited at touchdown, but are out of
phase with the touchdown-induced TMR, the PES generated by the
touchdown-induced TMR is cancelled. Consequently, TMR does not
increase at touchdown, thereby making touchdown detection by
observing PES variance with respect to total baseline PES
problematic. In the baseline RRO removal method, the synchronous
portion of the baseline PES, i.e., the baseline RRO, is quantified
and removed from the baseline PES measurement and the PES
measurements for each DFH power, so that touchdown-induced TMR is
essentially unaffected by the synchronous portion of the baseline
PES, i.e., baseline RRO.
[0043] FIG. 4 sets forth a flow diagram illustrating a baseline RRO
removal method 400 for determining touchdown of an R/W head against
a magnetic storage disk, according to an embodiment of the
invention. For ease of description, baseline RRO removal method 400
is described in terms of a disk drive substantially similar to disk
drive 110 in FIG. 1. However, other types of disk drives may also
benefit from the use of method 400. The commands for carrying out
steps 401-409 may reside in the disk drive control algorithm and/or
as values stored in the electronic circuits of the disk drive or on
the storage disk itself.
[0044] In step 401, the R/W head, such as R/W head 120 in FIG. 1,
is positioned at a maximum distance from a magnetic storage disk.
For disk drive 110, this is accomplished by reducing the DFH power
to zero, i.e., 0 DAC counts.
[0045] In step 402, disk drive 110 determines baseline PES by
measuring PES over one or more revolutions for one location on
magnetic storage disk 112.
[0046] In step 403, disk drive 110 determines baseline RRO, i.e.,
the synchronous portion of baseline PES, by synchronously averaging
the PES for multiple revolutions of storage disk 112. The same
measurements used to determine baseline PES in step 402 may also be
used for step 403. Alternatively, additional runs may be performed
to collect the requisite PES data for step 403.
[0047] In step 404, disk drive 110 removes the baseline RRO
determined in step 403 from the baseline PES determined in step 402
by subtracting the baseline RRO values from the baseline PES,
thereby producing an adjusted baseline PES.
[0048] In step 405, the adjusted baseline PES is converted into the
frequency domain by DFT methods commonly known in the art to
generate a baseline PES frequency distribution.
[0049] In steps 402-405 described above, the PES for multiple runs
of magnetic storage disk 112 is measured while R/W 120 is
positioned away from surface 112A of magnetic storage disk 112, and
the measured PES, after removal of the synchronous component, is
converted to the frequency domain by DFT or other known methods.
Thus, all PES measurements are taken with the DFH control signal at
zero DAC counts. In another embodiment, PES is measured and
averaged over multiple runs, where each run is performed with R/W
head 120 positioned at a slightly different height above surface
112A. For example, 10 runs may be used with DFH power at 0 DAC
counts for the first run, 1 DAC counts for the second run, 2 DAC
counts for the third run, and so on. Alternatively, a baseline PES
frequency distribution may based on the average of multiple runs,
where one or more of the runs with the greatest band-limited PES
variances and one or more of the smallest band-limited PES
variances are thrown out before averaging. Other suitable methods
of establishing a baseline PES frequency distribution may be
readily devised by one of skill in the art upon reading the
disclosure herein.
[0050] In step 406, the R/W head is stepped down one or more DAC
counts toward the surface of the disk. For maximum resolution of
touchdown, the R/W head is stepped down a single DAC count. Because
in some situations performing a PES measurement at each DAC count
may be overly time-consuming, the R/W may instead be stepped down
two or more DAC counts in step 406.
[0051] In step 407, the PES is measured at the new position of the
R/W head and the baseline RRO determined in step 403 is subtracted
from the measured PES, and the resultant PES is converted to the
frequency domain by DFT methods commonly known in the art.
[0052] In step 408, the PES variance at the current DAC count is
calculated by comparing the resultant PES frequency distribution
determined in step 407 with the baseline PES frequency distribution
determined in step 405. Only a limited portion of the PES frequency
distribution, e.g., 5000 Hz to 9000 Hz, is used to calculate the
PES variance.
[0053] A number of numerical methods may be used to determine the
PES variance in step 408. In one embodiment, the variance may be a
sum or the mean of the difference in PES magnitude (between the
resultant PES frequency distribution determined in step 407 with
the baseline PES frequency distribution determined in step 405) at
each frequency, squared. Alternatively, the total magnitude of the
resultant PES frequency distribution can be compared to the
magnitude of the baseline PES frequency distribution. Other methods
of calculating the variance can be readily devised by one of
ordinary skill in the art. However, summing the mean of the
difference in PES magnitude squared to quantify PES variance
advantageously increases the sensitivity of the touchdown detection
algorithm by including both amplitude increases and decreases of
the resultant PES frequency distribution relative to the baseline
PES frequency distribution. This is because some frequencies may
decrease below the baseline value due to damping and other effects
at initial touchdown. Thus, in some situations, the total PES
energy may not increase significantly when touchdown first occurs,
and a variance calculation based on the increase of the total PES
energy may delay declaration of touchdown. Equation 1 provides one
example of quantifying the variance of a measured PES spectrum at a
given DFH power, i.e., DAC count, from a baseline PES spectrum:
Var ( PES ) DAC .ident. 1 n j = 1 n ( PES j - PES BASELINE , j ) 2
Equation ( 1 ) ##EQU00001##
where n=the number of discrete frequencies measured in the PES
spectra; PES.sub.j=the magnitude of PES for each discrete
frequency, j; and PES.sub.BASELINE,j is the magnitude of the
baseline-PES at discrete frequency, j.
[0054] In step 409, touchdown determination is performed, i.e., the
PES variance calculated in step 408 is compared to the touchdown
criterion. In one embodiment, touchdown is declared when the PES
variance calculated in step 408 exceeds a specified quantity or
threshold value. In another embodiment, touchdown is declared when
the variance of the measured PES spectrum exceeds a specified
threshold value by a specified multiplicative factor, e.g., 1.5,
2.0, etc. If touchdown has not occurred, the process returns to
step 406. In yet another embodiment, touchdown is declared only
after the touchdown criterion is met for multiple consecutive DFH
powers, e.g., after the third consecutive DFH power. One of skill
in the art, upon reading the disclosure herein, can devise a
suitable selection criterion for declaring touchdown power based on
the design of a given disk drive and the process control
requirements for manufacturing the disk drive. In one embodiment,
one or more confirmation runs may also be performed once touchdown
is declared, in which the PES at the declared touchdown power is
re-measured. If touchdown has occurred, the process continues to
step 410. In step 410, touchdown is declared.
[0055] Method 400, as described above, would require storage of all
of the revolutions of measured PES, in order to allow subtraction
of the synchronous portion of the baseline PES before converting
into the frequency-domain. In alternative embodiments, it is
possible to store smaller amounts of data by keeping: (1) a running
total of the PES at each servo-wedge during the measurement for
determination of the synchronous portion of the PES; (2) the most
recent revolution of actual PES with which the band-limited PES
variance for that revolution can be computed after conversion into
the frequency domain; and (3) a running sum of the band-limited PES
variance. The band-limited PES variance with the synchronous
portion of the baseline PES removed can be estimated as the mean
band-limited PES variance minus the band-limited RRO variance,
where the mean band-limited PES variance is determined by dividing
the running sum of band-limited PES variances by the number of
revolutions of PES measured, and the band-limited RRO variance is
determined by transforming the synchronous portion of the PES into
the frequency domain and summing the squares of the selected
frequency components. This estimate can be made because the
expected value of the square of the sum (or difference) of two
independent random variables is equal to the sum (or difference) of
the expected values of the individual squares. In other words, the
expected value of (Total_PES-Synchronous_PES) 2 is estimated to be
equal to the expected value of Total_PES 2 minus the expected value
of Synchronous_PES 2.
[0056] FIG. 5A is a graph 500 of a series of PES frequency
distributions 501. Each of PES frequency distributions 501 is a DFT
of a PES produced during track following by R/W head 120, where
each PES frequency distribution 501 is taken at a different DFH
power. The horizontal axis of graph 500 represents the frequency of
the PES and has a range of 0 Hz to approximately 12,000 Hz, and the
vertical axis of graph 500 represents the scaled magnitude of PES
spectral components. In the example illustrated in FIG. 5A, PES
frequency distributions 501 end at approximately 12,000 Hz, which
is the Nyquist frequency of the disk drive being calibrated. The
frequency range examined is the range of frequencies from 6000 Hz
to the Nyquist frequency. The frequency and spectral magnitude for
all the spectra suffered by the drive for all the different DFH
powers are superimposed on each other in graph 500 to illustrate
where the spectra are the same and where they change at touchdown.
The high frequency spikes 509 occur at the highest DFH powers,
indicating touchdown. Touchdown in more clearly indicated in FIG.
5B.
[0057] FIG. 5B sets forth a graph 502 of band-limited PES variance
from a PES baseline measured against DFH power, in DAC counts,
where the PES variance at each DAC count is measured over a limited
portion of the frequency range and is calculated by the sum of the
squares of each frequency component. In the example illustrated in
FIG. 5B, the frequency range used to calculate variance for each
DAC count is the band between 6 kHz and the Nyquist frequency of
the PES, i.e., approximately 12,000 kHz. As shown, PES variance for
DAC counts up to about 85 is approximately the same, and the onset
of touchdown is clearly indicated at 90 DAC counts, when baseline
PES variance exceeds the threshold 503 of approximately 3000
units.
[0058] FIGS. 6A and 6B, when compared to FIGS. 5A and 5B,
respectively, illustrate the effectiveness of the baseline RRO
removal method 400 for determining touchdown of an R/W head. FIG.
6A is a graph 600 of a series of PES frequency distributions 601,
where the PES frequency distributions 601 are produced by
processing the PES frequency distributions 501 from graph 500 using
the baseline RRO removal method 400. Namely, the disk drive
determines the baseline synchronous RRO and subtracts the baseline
synchronous RRO from all PES measurements. Thus, the baseline RRO
has been removed from each of the spectra in graph 600, which
provides a more consistent result, and touchdown is more clearly
indicated. These improvements are illustrated in FIG. 6B.
[0059] FIG. 6B sets forth a graph 602 of band-limited PES variance
from a baseline PES having the baseline RRO removed, measured
against DFH power for the spectra in graph 600. Because the bulk of
the sum of the squares of the baseline spectrum is due to
synchronous runout, when the baseline RRO has been removed by the
baseline RRO removal method 400, the baseline 605 is substantially
lower in graph 602 than the baseline 505 in graph 502. Thus, the
signal-to-noise ratio of the calibration algorithm is substantially
improved over the algorithm used to generate graph 502. In
addition, because peak 606 in graph 602 is not substantially lower
than the corresponding peak in graph 502, it can be inferred that
at least some of the baseline RRO was actually canceling the
touchdown-induced TMR that produced the spectra in graph 500. In
contrast, if no cancellation had taken place, then peak 606 would
be reduced by approximately as much as baseline 605 is reduced
compared to baseline 505. One of skill in the art will appreciate
that for "noisier" drives, i.e., drives having a less clearly
defined baseline PES variance prior to touchdown, the removal of
TMR-canceling baseline RRO can make the difference between accurate
detection of touchdown and overdriving the R/W head past the point
of initial contact with the disk.
[0060] The band-limited RRO method for determining touchdown is now
described. Inventor analysis has determined that in some drives, a
significant quantity of non-synchronous runout (NRRO) may be
present in the frequencies of interest when trying to determine
touchdown. Thus, the relatively high amplitude NRRO, which cannot
be removed by baseline RRO removal method 400, can act as noise in
the frequencies at which touchdown-induced TMR occurs, thereby
masking the onset of touchdown. The band-limited RRO method, as
described herein, effectively removes the majority of NRRO that can
obscure the onset of touchdown.
[0061] FIG. 7 sets forth a flow diagram illustrating a band-limited
RRO method 700 for determining touchdown of an R/W head against a
magnetic storage disk, according to an embodiment of the invention.
For ease of description, band-limited RRO method 700 is described
in terms of a disk drive substantially similar to disk drive 110 in
FIG. 1, however other disk drives may also benefit from the use of
method 700. The commands for carrying out steps 701-707 may reside
in the disk drive control algorithm and/or as values stored in the
electronic circuits of the disk drive or on the storage disk
itself.
[0062] In step 701, steps 401-405 of method 400 are performed to
determine the baseline RRO, the adjusted baseline PES, and the
baseline PES frequency distribution.
[0063] In step 702, the R/W head is stepped down one or more DAC
counts toward the surface of the disk and a PES is measured for a
plurality of revolutions, e.g., 10, 20, etc. Measuring PES for a
larger number of revolutions will more completely remove the effect
of NRRO on the PES variance. In one embodiment, a larger number of
revolutions may be measured for a particular R/W head and/or
location of touchdown measurement that is known to be subject a
significant amount of NRRO, such as for an R/W head located between
tow storage disks and/or at the outer diameter of the disks. In
addition, for maximum resolution of touchdown, the R/W head is
stepped down a single DAC count. Because in some situations
performing a PES measurement at each DAC count may be overly
time-consuming, the R/W head may instead be stepped down two or
more DAC counts in step 702.
[0064] In step 703, the baseline RRO determined in step 701 is
subtracted from each PES measurement taken in step 702, in order to
remove the effect of synchronous runout present in the baseline
PES.
[0065] In step 704, each of the PES measurements modified in step
703 is then synchronously averaged over a number of revolutions of
storage disk 112, and the resultant PES is converted into the
frequency domain by DFT methods commonly known in the art.
[0066] In step 705, the PES variance at the current DAC count is
calculated by comparing the resultant PES frequency distribution
determined in step 704 with the baseline PES frequency distribution
determined in step 701. Different methods may be used to determine
the PES variance in step 705, and are set forth above in step 408
of baseline RRO removal method 400.
[0067] In step 706, touchdown determination is performed, i.e., the
PES variance calculated in step 705 is compared to the touchdown
criterion. Different methods may be used to determine the PES
variance in step 705, and are set forth above in step 409 of
baseline RRO removal method 400. If touchdown has not occurred, the
process returns to step 702. If touchdown has occurred, the process
continues to step 707. In step 707, touchdown is declared.
[0068] FIGS. 8A and 8B illustrate a graph 800 of PES frequency
distributions 801 and a graph 802 of band-limited PES variance
measured against DFH power, respectively, for a drive that
experiences a significant amount of high-frequency NRRO during the
calibration process. As shown, PES frequency distributions 801
produce a relatively high and "jittery" baseline 805, making a
reliable touchdown determination problematic. FIGS. 9A and 9B
illustrate a graph 900 of PES frequency distributions 901 and a
graph 902 of band-limited PES variance measured against DFH power,
respectively, for the same drive, where the PES frequency
distributions 901 are produced by processing the PES frequency
distributions 801 of FIG. 8A using the baseline RRO removal method
400. Due to the relatively large NRRO experienced by the drive,
baseline RRO removal method 400 only improves baseline 805
incrementally to baseline 905. FIGS. 10A and 10B illustrate a graph
1000 of PES frequency distributions 1001 and a graph 1002 of
band-limited PES variance measured against DFH power, respectively,
for the same drive, where the PES frequency distributions 1001 are
produced by processing the PES frequency distributions 801 of FIG.
8A using band-limited RRO method 700. In this case, the synchronous
averaging of band-limited RRO method 700 does an excellent job of
reducing the effects of NRRO, as evidenced by the low and constant
baseline 1005 in graph 1002. Baseline 1005 facilitates reliable
touchdown determination.
[0069] The slope method for determining touchdown is now described.
The slope method examines the difference between the average of a
PES variance metric at the beginning of touchdown determination and
the average of the PES variance metric at the most recently
measured DFH powers. Touchdown is declared when the difference
between these two averages exceeds a threshold value, rather than
by using a fixed threshold value for the PES metric itself. In one
embodiment, the PES variance as determined in step 408 of baseline
RRO removal method 400 is used as the PES variance metric. In
another embodiment, the PES variance as determined in step 705 of
band-limited RRO method 700 is used as the PES variance metric.
[0070] FIG. 11 sets forth a flow diagram illustrating a slope
method 1100 for determining touchdown of an R/W head against a
magnetic storage disk, according to an embodiment of the invention.
For ease of description, slope method 1100 is described in terms of
a disk drive substantially similar to disk drive 110 in FIG. 1,
however other disk drives may also benefit from the use of method
700. The commands for carrying out steps 1101-1105 may reside in
the disk drive control algorithm and/or as values stored in the
electronic circuits of the disk drive or on the storage disk
itself. It is noted that no additional measurements are necessary
to perform slope method 1100.
[0071] In step 1101, a baseline for the selected PES variance
metric is established by calculating the average value of the
metric for a specified number of measurements at the beginning of
the touchdown calibration, e.g., the first 10 or 20 DAC counts. In
one embodiment, the baseline for PES variance is a running average
of all PES variance values excluding the most recent values, which
are averaged in step 1103, below. In such an embodiment, the
baseline PES variance is updated with each DFH power. The metric
used for slope method 1100 may be the PES variance for a given DFH
power as measured by either baseline RRO removal method 400 or by
band-limited RRO method 700.
[0072] In step 1102, a threshold value for declaring touchdown is
determined. Touchdown is declared (in step 1105) when the average
value of the most recent PES variance measurements exceeds the
average baseline value for the PES variance by the threshold value.
In one embodiment, the threshold value is a function of the history
of the metric used and can change with each DFH power at which PES
variance is measured.
[0073] In step 1103, the values of the most recent PES variance
measurements are averaged. In one embodiment, the 10 most recent
PES variance measurements are used. It is contemplated that the
number of PES variance measurements averaged in step 1103 may be
greater or less than 10. However, averaging too few measurements
may result in early touchdown declaration due to a few noisy
samples, and averaging too many measurements may result in late
touchdown declaration.
[0074] In step 1104, touchdown determination is performed, i.e.,
the average PES variance of the most recent PES variance
measurements, e.g., the latest 10 DAC counts, is compared to the
average baseline PES variance. Touchdown occurs when the difference
exceeds the threshold value selected in step 1102. If touchdown has
not occurred, the R/W head is stepped down with, the next DFH power
and the process returns to step 1101. If touchdown has occurred,
the process continues to step 1105. In step 1105, touchdown is
declared.
[0075] In one embodiment, touchdown cannot be declared below a
specified number of DAC counts, for example 60 DAC counts. The
minimum DAC count specified may be varied as a function of what
model of drive or R/W head location is undergoing the touchdown
calibration.
[0076] In one embodiment, the threshold determined in step 1102 may
be increased with each DFH power so that the threshold remains a
specified factor above the running baseline value. For example, if
the difference calculated in step 1104 does not exceed but is
greater than half the threshold, the threshold may be increased to
twice the difference determined in step 1104. In one embodiment,
there may be a maximum number of DAC counts specified, after which
the threshold will not be increased regardless of the value of the
difference calculated in step 1104.
[0077] FIG. 12 sets forth a graph 1200 that illustrates the output
of slope method 1100 using the data from graph 1002 in FIG. 10B,
which is a graph of band-limited PES variance measured against DFH
power as determined by band-limited RRO method 700. Considering
that graph 1002 was generated from a "noisy" drive, as illustrated
by the PES variance illustrated in FIG. 8B, graph 1200 indicates
that slope method 1100 also works well in determining touchdown for
a less than ideal drive.
[0078] Baseline RRO removal method 400, band-limited RRO method
700, and slope method 1100 may be performed in a conventional test
environment, i.e., in a manufacturing setting. However, because no
additional measuring equipment is required for disk drive to
perform the above methods, a disk drive may also perform such
methods whenever it may be deemed necessary. For example, a disk
drive may perform baseline RRO removal method 400, band-limited RRO
method 700, and/or slope method 1100 on one or more tracks upon
each start-up of the drive, or periodically throughout the life of
the drive. Alternatively, a drive may perform said methods on one
or more tracks under specific circumstances, e.g., whenever the
drive reaches a certain temperature, or as a part of an
error-recovery algorithm.
[0079] The use of PES variance, as described herein, provides a
number of advantages over methods known in the art for determining
touchdown. First, no external equipment is required for disk drive
to perform touchdown determination. Second, as illustrated by FIGS.
6A, 6B, 9A, 9B, and 12, a touchdown determination algorithm based
on the methods disclosed herein provides a reliable method for
detecting touchdown, even for drives experiencing significant
baseline RRO and/or high-frequency NRRO. Third, minimal head/disk
contact is required.
[0080] While the foregoing is directed to embodiments of the
present invention, other and further embodiments of the invention
may be devised without departing from the basic scope thereof, and
the scope thereof is determined by the claims that follow.
* * * * *